Aerospace series - Titanium tube for 35 MPa operating pressure - Part 1: Inch series

ISO 18487-1:2017 is applicable to seamless tubing of circular cross-section made from titanium alloy and intended for use primarily in systems with system operating pressure of 35 MPa (5 080 psi) (Pressure Class J), but usage is not limited to such applications.

Série aérospatiale — Tubes en titane — Pression de service : 35 MPa — Partie 1: Série en inches

General Information

Status
Published
Publication Date
24-Apr-2017
Current Stage
9599 - Withdrawal of International Standard
Start Date
02-Jul-2025
Completion Date
13-Dec-2025
Ref Project

Relations

Overview

ISO 18487-1:2017 - "Aerospace series - Titanium tube for 35 MPa operating pressure - Part 1: Inch series" - is an international standard that defines technical requirements for seamless titanium alloy tubing used primarily in aerospace systems rated for 35 MPa (5 080 psi, Pressure Class J). The document harmonizes dimensions, materials, manufacturing and test requirements for inch-series tube sizes commonly used in hydraulic and fluid systems in aircraft and space vehicles.

Key topics and technical requirements

  • Scope and applicability: Seamless circular titanium tubing intended for systems with 35 MPa operating pressure, but not restricted to those applications.
  • Dimensions and tolerances: Nominal inch-series sizes are specified with SI units; dimensional requirements reference ISO 8575 and tolerances reference ISO 12573.
  • Chemical composition: Composition limits are defined for alloying elements and impurities. Example ranges include Al 2.50–3.50%, V 2.00–3.00%, with strict limits on interstitials (O ≤ 0.120%, N ≤ 0.020%, H ≤ 0.005%). Analytical methods (ASTM/EN) are referenced.
  • Melting practice: Multiple melts with inert gas flooding are required; open-air furnace melting is not permitted. Vacuum arc remelting (VAR) is required for second and subsequent melts.
  • Heat treatment and delivery condition: Cold-worked, stress-relieved in vacuum or inert atmosphere at a minimum of 370 °C for 30 minutes; rotary straightening after final heat treatment is not permitted.
  • Mechanical properties: Tensile testing at 15 °C with specified tensile strength, 0.2% proof stress and elongation criteria (see Table 2 in the standard). Sample size and reporting requirements are specified.
  • Microstructure and CSR: Microstructure inspection (≥400×) and grain-size determination per ASTM E112; Contractile Strain Ratio (CSR) when required shall be between 1.3 and 3.5 (AS 4076 method).
  • Surface condition: OD chemical milling to remove at least 0.025 mm; ID chemical milling minimum 0.013 mm. Surface texture and ultrasonic inspection requirements are included.
  • Testing: Includes ultrasonic inspection, flarability, bending, flattening, deformation-under-pressure, impulse pressure-fatigue (proof and pressure-impulse tests), and ultimate/burst testing as referenced.

Practical applications and users

  • Primary users: aerospace OEMs, tubing manufacturers, suppliers of hydraulic tubing, aircraft maintenance organizations, quality and test laboratories, procurement/specification engineers.
  • Applications: high-pressure aircraft hydraulic lines, aerospace fluid systems, pressure-critical tubing in landing gear, flight control actuators and other systems requiring lightweight, high-strength, corrosion-resistant tubing at 35 MPa.

Related standards (selected)

  • ISO 8575 (aerospace hydraulic tubing dimensions)
  • ISO 12573 (tubing tolerances - inch series)
  • ISO 4287 (surface texture)
  • ISO 6772, ISO 10583 (impulse testing and test methods)
  • AS 4076, ASTM E112, EN 2003-010 (test methods and material analysis)

Keywords: ISO 18487-1, titanium tube, 35 MPa, aerospace tubing, pressure class J, seamless tubing, tensile properties, chemical composition, impulse pressure fatigue.

Standard
ISO 18487-1:2017 - Aerospace series -- Titanium tube for 35 MPa operating pressure
English language
13 pages
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Standards Content (Sample)


INTERNATIONAL ISO
STANDARD 18487-1
First edition
2017-04
Aerospace series — Titanium tube for
35 MPa operating pressure —
Part 1:
Inch series
Série aérospatiale — Tubes en titane — Pression de service : 35 MPa —
Partie 1: Série en inches
Reference number
©
ISO 2017
© ISO 2017, Published in Switzerland
All rights reserved. Unless otherwise specified, no part of this publication may be reproduced or utilized otherwise in any form
or by any means, electronic or mechanical, including photocopying, or posting on the internet or an intranet, without prior
written permission. Permission can be requested from either ISO at the address below or ISO’s member body in the country of
the requester.
ISO copyright office
Ch. de Blandonnet 8 • CP 401
CH-1214 Vernier, Geneva, Switzerland
Tel. +41 22 749 01 11
Fax +41 22 749 09 47
copyright@iso.org
www.iso.org
ii © ISO 2017 – All rights reserved

Contents Page
Foreword .iv
Introduction .v
1 Scope . 1
2 Normative references . 1
3 Terms and definitions . 2
4 Dimensions . 2
5 Tolerances . 3
6 Technical requirements . 3
6.1 General . 3
6.2 Composition . 3
6.3 Melting practice . 3
6.4 Heat treatment and delivery condition . 3
6.5 Tensile properties . 3
6.6 Microstructure . 4
6.6.1 General. 4
6.6.2 Grain size . 4
6.6.3 Contractile strain ratio (CSR) . 4
6.7 Surface condition and texture . 4
6.7.1 Surface treatment. 4
6.7.2 Surface condition . 4
6.7.3 Surface texture, R .
a 5
6.8 Ultrasonic inspection . 5
6.9 Flarability . 5
6.9.1 General. 5
6.9.2 Surface contamination . 5
6.10 Bending . 7
6.11 Flattening . 7
6.12 Deformation under pressure test . 7
6.13 Impulse pressure fatigue test . 8
6.13.1 General. 8
6.13.2 Proof test. 8
6.13.3 Pressure impulse test . 8
6.13.4 Additional test .11
6.13.5 Ultimate (as per CS 25.1435) and burst test.11
7 Quality assurance .12
8 Preparation for delivery .12
8.1 Marking .12
8.2 Packing .12
Bibliography .13
Foreword
ISO (the International Organization for Standardization) is a worldwide federation of national standards
bodies (ISO member bodies). The work of preparing International Standards is normally carried out
through ISO technical committees. Each member body interested in a subject for which a technical
committee has been established has the right to be represented on that committee. International
organizations, governmental and non-governmental, in liaison with ISO, also take part in the work.
ISO collaborates closely with the International Electrotechnical Commission (IEC) on all matters of
electrotechnical standardization.
The procedures used to develop this document and those intended for its further maintenance are
described in the ISO/IEC Directives, Part 1. In particular the different approval criteria needed for the
different types of ISO documents should be noted. This document was drafted in accordance with the
editorial rules of the ISO/IEC Directives, Part 2 (see www .iso .org/ directives).
Attention is drawn to the possibility that some of the elements of this document may be the subject of
patent rights. ISO shall not be held responsible for identifying any or all such patent rights. Details of
any patent rights identified during the development of the document will be in the Introduction and/or
on the ISO list of patent declarations received (see www .iso .org/ patents).
Any trade name used in this document is information given for the convenience of users and does not
constitute an endorsement.
For an explanation on the voluntary nature of standards, the meaning of ISO specific terms and
expressions related to conformity assessment, as well as information about ISO’s adherence to the
World Trade Organization (WTO) principles in the Technical Barriers to Trade (TBT) see the following
URL: w w w . i s o .org/ iso/ foreword .html
This document was prepared by Technical Committee ISO/TC 20, Aircraft and space vehicles,
Subcommittee SC 10, Aerospace fluid systems and components.
A list of all the parts in the ISO 18487 series can be found on the ISO website.
iv © ISO 2017 – All rights reserved

Introduction
This document is intended to harmonize the technical requirements for titanium tubes used in
aerospace with design operating pressure of 35 MPa.
It is noted that, while ISO standards should normally refer only to SI units, large segments of the
aerospace industry refer to other measurement systems as a matter of common working practice. The
mention of “inch series” in the title of this document reflects this. It recognizes the fact that the nominal
sizes referred to in the document, which are in common use in the aerospace industry, were originally
defined in terms of fractional inches.
Although the tube sizes were originally defined, and are frequently referred to, in terms of non-SI units,
all dimensions used in this document are in SI units with inch units given in addition for the convenience
of those users more familiar with these.
It is further noted that the standard ISO decimal symbol “,” (comma) is not used as common working
practice for inch dimensions. A decimal point is used in the inch dimensions in this document as in
many other aerospace standards.
NOTE The use of non-SI units and the decimal point in this document does not constitute general acceptance
of measurement systems other than SI within International Standards.
INTERNATIONAL STANDARD ISO 18487-1:2017(E)
Aerospace series — Titanium tube for 35 MPa operating
pressure —
Part 1:
Inch series
1 Scope
This document is applicable to seamless tubing of circular cross-section made from titanium alloy and
intended for use primarily in systems with system operating pressure of 35 MPa (5 080 psi) (Pressure
Class J), but usage is not limited to such applications.
2 Normative references
The following documents are referred to in the text in such a way that some or all of their content
constitutes requirements of this document. For dated references, only the edition cited applies. For
undated references, the latest edition of the referenced document (including any amendments) applies.
ISO 4287, Geometrical Product Specifications (GPS) — Surface texture: Profile method — Terms, definitions
and surface texture parameters
ISO 6772, Aerospace — Fluid systems — Impulse testing of hydraulic hose, tubing and fitting assemblies
ISO 8492, Metallic materials — Tube — Flattening test
ISO 8575:2016, Aerospace — Fluid systems — Hydraulic system tubing
ISO 10583, Aerospace fluid systems — Test methods for tube/fitting assemblies
ISO 12573, Aircraft — Tubing tolerances — Inch series
EN 2003-010, Aerospace series — Titanium and titanium alloys — Test methods — Part 010: Sampling for
determination of hydrogen content
EN 3718, Aerospace series — Test method for metallic materials — Ultrasonic inspection of tubes
AS 4076, Contractile strain ratio testing of titanium hydraulic tubing
AMS 2634, Ultrasonic inspection, thin wall metal tubing superseding
ASTM E112, Standard test methods for determining average grain size
ASTM E1409, Standard test method for determination of oxygen and nitrogen in titanium and titanium
alloys by inert gas fusion
ASTM E1941, Standard test method for determination of carbon in refractory and reactive metals and their
alloys by combustion analysis
ASTM E1447, Standard test method for determination of hydrogen in titanium and titanium alloys by the
inert gas fusion thermal conductivity/infrared detection method
ASTM E2371, Standard test method for analysis of titanium and titanium alloys by direct current plasma
and inductively coupled plasma atomic emission spectrometry (Performance-based test methodology)
3 Terms and definitions
For the purposes of this document, the following terms and definitions apply.
ISO and IEC maintain terminological databases for use in standardization at the following addresses:
— IEC Electropedia: available at http:// www .electroped
...

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Frequently Asked Questions

ISO 18487-1:2017 is a standard published by the International Organization for Standardization (ISO). Its full title is "Aerospace series - Titanium tube for 35 MPa operating pressure - Part 1: Inch series". This standard covers: ISO 18487-1:2017 is applicable to seamless tubing of circular cross-section made from titanium alloy and intended for use primarily in systems with system operating pressure of 35 MPa (5 080 psi) (Pressure Class J), but usage is not limited to such applications.

ISO 18487-1:2017 is applicable to seamless tubing of circular cross-section made from titanium alloy and intended for use primarily in systems with system operating pressure of 35 MPa (5 080 psi) (Pressure Class J), but usage is not limited to such applications.

ISO 18487-1:2017 is classified under the following ICS (International Classification for Standards) categories: 49.080 - Aerospace fluid systems and components. The ICS classification helps identify the subject area and facilitates finding related standards.

ISO 18487-1:2017 has the following relationships with other standards: It is inter standard links to ISO 19363:2020, ISO 18487-1:2025. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

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